A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is developed. The method utilizes the interface shock spectra and the relative impedance of the spacecraft and launch vehicle. The method is developed for single-degree-of-freedom models and then generalized to multidegree-of-freedom models. (Author)


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    Titel :

    A Shock Spectra and Impedance Method to Determine a Bound for Spacecraft Structural Loads


    Beteiligte:
    R. Bamford (Autor:in) / M. Trubert (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch